Aircraft Design Projects Episode 13 pot

... 312 Flying car 177 HALE aircraft 275 Design course aims 353 Design flexibility 3 Design flowchart 7 Design meetings 338 Design organisation 10 Design presentations 349 Design process 1 Design requirements: Biz ... 75 AIAA Student Design Competition 203 Aircraft balance 21 Amphib. aircraft 319 HALE aircraft 297 Mil. bomber 233 Aircraft development programmes 15 Aircr...

Ngày tải lên: 13/08/2014, 15:21

... that loading the aircraft from the operational empty mass will progressively move the aircraft centre of gravity forward, “chap02” — 2003/3/10 — page 18 — #13 18 Aircraft Design Projects a – ... — #9 14 Aircraft Design Projects 2.3.4 Commercial and manufacturing considerations Political issues may affect the way in which the aircraft is to be manufactured. Large aircr...

Ngày tải lên: 13/08/2014, 15:21

... “chap06” — 2003/3/10 — page 170 — #28 170 Aircraft Design Projects weight gives the max. climb performance of the aircraft at constant aircraft forward speed (i.e. with zero acceleration). The ... 1-56347-250-3. 8 Tully, C., Aircraft conceptual design workbooks’, Final-year project study, Loughborough University, May 2001. “chap07” — 2003/3/10 — page 180 — #6 180 Aircraft Desi...

Ngày tải lên: 13/08/2014, 15:21

... changes to the aircraft configuration will affect both aircraft selling price and operating costs. For civil aircraft designs, these two cost parameters are often selected as the principal design drivers ... cent of aircraft design mass → 900 kg Crew: Assume one pilot with operational equipment → 300 lb = 136 kg Weapon load: Specified at 3000 lb → 136 0 kg Hence the initial mass s...

Ngày tải lên: 08/08/2014, 11:21

Ngày tải lên: 13/08/2014, 05:20

... Wing fuel volume 133 5.10 Further work 134 5.11 Study review 137 5.11.1 Strengths 137 5.11.2 Weaknesses 137 5.11.3 Opportunities 139 5.11.4 Threats 139 5.11.5 Revised aircraft layout 140 ... distance 130 5.8.4 Fundamental flight analysis 130 5.8.5 Combat turns at SL 130 5.8.6 Combat turn at 25 000 ft 131 5.8.7 Climb rate 131 5.8.8 Constraint diagram 131 5.9 Revised...

Ngày tải lên: 13/08/2014, 15:21

... studies For any aircraft design, it is uncommon to consider just the capability of the aircraft at the design point. Trading fuel for payload with the aircraft kept at the max. design mass results ... depreciation costs of owning the aircraft. On this aircraft, this would be about 33 per cent of the total DOC. If the aircraft operator leases the aircraft, the annual cost of t...

Ngày tải lên: 13/08/2014, 15:21

... load the aircraft take-off mass will be 5707 kg. To account for the weapon drag the lift/drag ratio will be reduced to 7.5. “chap05” — 2003/3/10 — page 130 — #30 130 Aircraft Design Projects 5.8.3 ... super- sonic aircraft are above this line and older aircraft substantially below. This reflects the “chap05” — 2003/3/10 — page 113 — #13 Project study: military training system 1...

Ngày tải lên: 13/08/2014, 15:21

... aircraft design and performance: 1 Raymer, D. P., Aircraft Design: A Conceptual Approach, AIAA Education Series, 1999, ISBN 1-56347-281-0. “chap05” — 2003/3/10 — page 132 — #32 132 Aircraft Design ... modified engine if the electric system is “chap05” — 2003/3/10 — page 138 — #38 138 Aircraft Design Projects This would allow the design and validation of the ground-based...

Ngày tải lên: 13/08/2014, 15:21